Fluid Mechanics |
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Page 478
... velocity v2 with which the flame moves relative to gas 2 is then determined at once by the condition ( 120.3 ) . At the closed end of the pipe , the gas velocity must vanish , and so the gas in region 2 will be at rest . Gas 1 ...
... velocity v2 with which the flame moves relative to gas 2 is then determined at once by the condition ( 120.3 ) . At the closed end of the pipe , the gas velocity must vanish , and so the gas in region 2 will be at rest . Gas 1 ...
Page 487
... gas in front of it , with a velocity exceeding c2 , and the latter with a velocity equal to c2 , and either would overtake the detonation wave . Thus , on the above assumption , the velocity of the gas moving behind the detona- tion ...
... gas in front of it , with a velocity exceeding c2 , and the latter with a velocity equal to c2 , and either would overtake the detonation wave . Thus , on the above assumption , the velocity of the gas moving behind the detona- tion ...
Page 492
... velocity v1 of the detonation wave relative to the gas at rest in front of it , and its velocity v relative to the burnt gas just behind it , are given in terms of the temperature T1 by formulae ( 121.11 ) , ( 121.12 ) . v , is also the ...
... velocity v1 of the detonation wave relative to the gas at rest in front of it , and its velocity v relative to the burnt gas just behind it , are given in terms of the temperature T1 by formulae ( 121.11 ) , ( 121.12 ) . v , is also the ...
Contents
3 Hydrostatics | 7 |
10 Incompressible fluids | 27 |
11 The drag force in potential flow past a body | 35 |
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Common terms and phrases
adiabatic amplitude angle axis Bernoulli's equation body boundary conditions boundary layer calculation characteristics co-ordinates coefficient combustion constant corresponding cross-section cylinder denote derivative determined detonation wave dimension direction distance drag energy flux entropy equation of continuity equations of motion equilibrium Euler-Tricomi equation Euler's equation expression flow past fluid velocity flux density formula frequency function gas velocity given gives grad gradient heat Hence ideal fluid incompressible increases infinity integral intersection Laplace's equation M₁ mechanical equilibrium moves Navier-Stokes equation obtain oscillations p₁ parameters perturbations pipe plane potential flow pressure PROBLEM propagated quantities radius rarefaction wave result Reynolds number shock wave simple wave small compared solution sound wave sphere spherical streamlines subsonic Substituting superfluid supersonic surface of discontinuity temperature tensor thermal conduction thermodynamic turbulent flow v₁ v₂ vector velocity component velocity of sound viscosity volume weak discontinuity x-axis zero др дх дхк
References to this book
Level Set Methods and Dynamic Implicit Surfaces Stanley Osher,Ronald Fedkiw No preview available - 2002 |